公开(公告)号：US20180363319A1

公开(公告)日：2018-12-20

申请号：US16012241

申请日：2018-06-19

Applicant: Airbus SAS ,  Airbus Operations SAS

Inventor： Jean-Claude MARTY ,  Julien CHARLES ,  Olivier LEBAHAR ,  Franck DOBIGEON ,  Guillaume FERRER ,  Thierry BORJA ,  Sebastien HANSER

IPC: E04H15/20 ,  B29C73/02 ,  B05D3/02 ,  B05D3/04 ,  B05D5/00 ,  B29C73/34

CPC classification number: E04H15/20 ,  B05D3/0254 ,  B05D3/0413 ,  B05D5/005 ,  B29C73/02 ,  B29C73/34 ,  B29L2031/3082 ,  B64C1/06 ,  E04H2015/201

Abstract: A method for repairing a structure comprising at least one zone to be heated and which comprises the steps of inflating a frame to form a framework, attaching panels removably to the frame to form an enclosure referred to as a heating enclosure, positioning the enclosure over the zone, heating the interior space of the enclosure using a heating device.

公开(公告)号：US20190337578A1

公开(公告)日：2019-11-07

申请号：US16400438

申请日：2019-05-01

Applicant: Airbus SAS

Inventor： Julien CHARLES ,  Guillaume FERRER

IPC: B62D41/00 ,  B60R19/20 ,  B60R19/48

Abstract: A vehicle bumper comprising at least one part made of resilient material, in the interior of which there is provided at least one marking fluid cell with an opening to the exterior. The opening is closed by a closure device which, under the effect of a pressure applied with a determined intensity, can open up the opening, allowing the marking fluid to access the exterior of the cell through which the marking fluid can flow, and also comprising a securing element configured to secure the at least one part on the vehicle.

公开(公告)号：US20190339297A1

公开(公告)日：2019-11-07

申请号：US16400417

申请日：2019-05-01

Applicant: Airbus SAS

Inventor： Julien CHARLES ,  Guillaume FERRER

IPC: G01P1/07 ,  B60R19/02 ,  B60R19/03 ,  G01P1/12

Abstract: A bumper for a vehicle, comprising at least one part made of resilient material, having a curved front portion forming an inner cavity. The front portion has apertures enabling the cavity to be put into communication with the exterior of the resilient part. At least one marking fluid cell is provided inside the cavity. A fastener is provided to fasten the one part to the vehicle.

公开(公告)号：US20170028655A1

公开(公告)日：2017-02-02

申请号：US15216914

申请日：2016-07-22

Applicant: Airbus SAS ,  Airbus Operations SAS

Inventor： Guillaume FERRER ,  Thierry BORJA ,  Julien CHARLES

IPC: B29C73/08 ,  B29C73/06

CPC classification number: B29C73/08 ,  B29C73/06 ,  B29C73/12 ,  B29C73/30 ,  B29L2031/3076

Abstract: A method and a tool for repairing a composite-material panel of an aircraft with at least one repair part made of composite material without using an autoclave. The repair method includes the steps of preparing the panel, placing at least one repair part made of composite material on the second face to cover a damaged zone, positioning a vacuum bag configured to sealingly cover the repair part, polymerizing or consolidating the repair part, compressing the vacuum bag against the repair part using a compression plate concomitantly with the step in which the repair part is polymerized or consolidated.

Abstract translation: 一种用于使用至少一个由复合材料制成的修复部件来修复飞行器的复合材料面板而不使用高压釜的方法和工具。 该修复方法包括以下步骤：制备面板，将至少一个由复合材料制成的修复部件放置在第二面上以覆盖受损区域，定位真空袋，以密封地覆盖修复部件，聚合或固结修复部件， 使用压缩板将真空袋压靠在修理部件上，同时与修复部件聚合或固结的步骤相对应。